CN1903552A - In-mould clad material forming method, and method for manufacturing clad material integrated shaped product - Google Patents
In-mould clad material forming method, and method for manufacturing clad material integrated shaped product Download PDFInfo
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- CN1903552A CN1903552A CNA2006101038105A CN200610103810A CN1903552A CN 1903552 A CN1903552 A CN 1903552A CN A2006101038105 A CNA2006101038105 A CN A2006101038105A CN 200610103810 A CN200610103810 A CN 200610103810A CN 1903552 A CN1903552 A CN 1903552A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C51/00—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
- B29C51/16—Lining or labelling
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/12—Moulds or cores; Details thereof or accessories therefor with incorporated means for positioning inserts, e.g. labels
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2791/00—Shaping characteristics in general
- B29C2791/004—Shaping under special conditions
- B29C2791/006—Using vacuum
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C51/00—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
- B29C51/10—Forming by pressure difference, e.g. vacuum
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C51/00—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
- B29C51/12—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor of articles having inserts or reinforcements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C51/00—Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
- B29C51/26—Component parts, details or accessories; Auxiliary operations
- B29C51/30—Moulds
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
An in-die cover forming method for integrally forming a cover member with a surface of a base member in a die is provided. The die including an upper die half and a lower die half. The upper die halves are movable relative to each other. The base member is set on the lower die half such that its back is opposed to the lower die half. Using position determining mechanisms located between the lower die half and the back of the base member, the position of the surface of the base member in relation to the lower die half in the die moving direction is determined. The cover member is placed between the base member and the upper die half. The cover member is integrated with the surface of the base member by closing the upper die half with respect to the lower die half while pressing the cover member against the base member through vacuuming.
Description
Technical field
The present invention relates to a kind of in-mould clad material formation method, wherein the surface of cover material and base material forms as one in mould, the invention still further relates to a kind of method that is used for making by this in-mould clad material formation method clad material integrated shaped product.
Background technology
Usually has the combination with decorative surfaces of making by cladding material such as internal parts such as the side plate of console and lid, instrument board, instrument case lids, so that these parts have the high-quality outward appearance.As shown in Figure 3, when making this internal part 80, resin base material 81 and cover material spare 82 are placed in the mould 90.Then, when being pressed against cover material spare 82 on the base material 81 by application of vacuum, closed mold 90.Thereby cover material spare 82 is combined into one with the surface of base material 81.The method is called in-mould clad material formation method.The mould 90 that is used for this formation method comprises upper mold section 90a and female die 90b.Upper mold section 90a has the cavity surface corresponding to base material 81 surface configurations.Female die 90b has the cavity surface corresponding to base material 81 back side shapes.
As shown in Figure 3, internal part 80 has reinforcement 81c and sidewall 81b.As shown in the right half part of Fig. 3, when using mould 90 to make internal part 80, the back side shape of the base material 81 that comprises reinforcement 81c and sidewall 81b is conformed to the shape of female die 90b.In other words, base material 81 is placed on the female die 90b, and determines the position of base material 81 at vertical and horizontal.The direction that half module 90a, 90b move relative to each other (that is seen in Fig. 3 is vertical) in perpendicular plane, is determined vertical and horizontal.
Subsequently, the cover material spare 82 that heats and soften is placed on the surface of base material 81, and upper mold section 90a is placed on the upper surface of cover material spare 82.After this, by application of vacuum, draw cover material spare 82 from the cavity surface side draught of female die 90b, so that cover material spare 82 tight contact substrates 81.At last, by closed mold 90, cover material spare 82 is bonded on the surface of base material 81.Usually, use adhesive that cover material spare 82 is bonded on the base material 81.
Usually, the combination with decorative surfaces of internal part 80 has a large amount of curve forms, to provide the high-quality outward appearance.Smooth cover material spare 82 is difficult to combine with the parts with this three-dimensional structure.Therefore, can cause defective.For example, have such situation, cover material spare 82 is from the displacement suitable with respect to base material 81, perhaps cover material spare 82 local bucklings.For addressing this is that, for example Japanese publication bulletin No.7-205167 has proposed wherein to use the in-mould clad material formation method of fixture.The fixture that bulletin discloses among the No.7-205167 comprises the actuator that respectively has actuator lever at the periphery of upper mold section.When opening mould, actuator lever is moved to female die.When closed mold, actuator lever moves down, so that this actuator lever extrudes and fixes the cover material spare that is placed on the female die at periphery.Along with the closure of mould, actuator lever is withdrawn because of the female die applied pressure.
On the other hand, Japanese publication bulletin No.2001-179759 has disclosed the method that is used for forming by bonding goods.In this method, be compressed against on the core with curved shape at the cover material spare that is formed with adhesive layer on its back side.After this, will turn back, with the back side of contact core at the folded part of cover material spare periphery.This formation method has following feature.That is, when using mould to be pressed against cover material spare on the whose surfaces,, make the attachment function of adhesive layer temporarily descend to the back side of folded part Jia Shui.Then, the heating folded part, so that this part is recovered adhesive function, and spine folded along core.
Smooth cover material spare 82 is combined with base material 81, so that cover material spare 82 conforms to the surface of the base material 81 with 3D shape, as mentioned above, it is difficult to handle.Like this, simply by determine the position of base material 81 at vertical and horizontal, perhaps, can not fully improve productive rate by suppressing the displacement of cover material spare 82 with respect to female die 90b with respect to female die 90b.Particularly, if base material 81 has elongated shape, then base material 81 might be in warpage after the injection moulding.This has just produced the variation of dimensional accuracy.As being schematically shown among Fig. 3, when using base material 81 to carry out in-mould clad material formation method, an end of base material 81 might separate from female die 90b.This can make cover material spare 82 fold or fracture.Therefore, need such technology, that is, can change the defective that takes place by the dimensional accuracy that reduces owing to base material 81, thereby significantly improve productive rate.
Summary of the invention
Therefore, the object of the present invention is to provide a kind of in-mould clad material formation method and a kind of method that is used to make clad material integrated shaped product, this method improves productive rate by reducing the generation defective.
For reaching aforementioned purpose, according to an aspect of the present invention, provide a kind of and be used for making the cover material spare and the surface of base material to form the in-mould clad material formation method of one at mould.Mould comprises first module and second module.One of at least the first module and second module can move with respect to another at the mould moving direction.In-mould clad material formation method comprises: on second module base material is set, makes that the back side of base material is relative with second module; When base material is set,, the surface of base material is located with respect to second module at the mould moving direction by the detent mechanism between the back side of second module and base material; Cover material spare is placed on first module and is located between the base material on second module; And, by application of vacuum cover material spare is pressed against on the base material, simultaneously,, the cover material spare and the surface of base material are combined into one by with respect to closed first module of second module.
According to a further aspect in the invention, provide a kind of method that is used to make clad material integrated shaped product, wherein, cover material spare is combined into one with the surface of base material.Described method comprises makes the cover material spare and the surface of base material form one in mould.Mould comprises first module and second module.One of at least the first module and second module can move with respect to another.Cover material spare comprises with the surface formation one of base material: on second module base material is set, makes that the back side of base material is relative with second module; When base material is set, engage with locking protuberance on being located at second module by making the engaging claw on the back side that is located at base material, the surface of base material is located with respect to second module; Cover material spare is positioned over first module and is located between the base material on second module; And, by application of vacuum cover material spare is pressed against on the base material, simultaneously,, the cover material spare and the surface of base material are combined into one by with respect to closed first module of second module.Described method also comprises, under the state by the fixture support substrate backside, repairs the edge of cover material spare along the peripheral part of base material.Anchor clamps comprise the lock pawl that can engage with engaging claw.In dressing process, engage with lock pawl by making engaging claw, with respect to anchor clamps location base material.
In conjunction with the drawings, with way of example principle of the present invention is carried out following explanation, other aspects and advantages of the present invention will be more clear.
Description of drawings
By the following explanation and the accompanying drawing of reference this paper preferred embodiment, the present invention may be better understood and purpose and advantage, in the accompanying drawings,
Figure 1A is the shaft side figure that the back side of clad material integrated shaped product is shown;
Figure 1B is the cutaway view along the line 1B to 1B of Figure 1A, and the base material that is placed on the mould and the part of cover material spare are shown;
Fig. 1 C is the cutaway view along the line 1C to 1C of Figure 1A, and the base material that is placed on the mould and the part of cover material spare are shown;
Fig. 2 is the cutaway view that schematically shows trim process; And
Fig. 3 is the cutaway view that schematically shows the technology of prior art in-mould clad material formation method.
The specific embodiment
To describe the manufacture method of clad material integrated shaped product according to an embodiment of the invention now.
Figure 1A is the shaft side figure that the back side of clad material integrated shaped product 10 is shown, and these goods are by prepared in accordance with the method for the present invention.One goods 10 comprise the resin base material 11 that forms by injection moulding.Base material 11 comprises rectangular plate shape upper wall 11a, extends and the reinforcement 11c of formation lattice downwards from the peripheral sidewall 11b that extends downwards of upper wall 11a with from the back side of upper wall 11a.Sidewall 11b opens to the lower end.
The surface of one goods 10 (combination with decorative surfaces) is coated with the lip-deep cover material spare 12 that is bonded to the top of upper wall 11a and sidewall 11b.Along the lower end of sidewall 11b, cover material spare 12 has folded part 12a.Folded part 12a is inwardly folding, and is bonded on the one goods 10.With adhesive cover material spare 12 is bonded on the base material 11.
As shown in Figure 1A and Figure 1B, engage each corner that protuberance 13 is located at the upper wall 11a back side.Triangle stiffener 16 is located at the base end part that respectively engages protuberance 13, so that protuberance 13 is connected with the back side of upper wall 11a.Each stiffener 16 has increased the intensity of re-spective engagement protuberance 13.Each stiffener 16 forms in vertical end towards base material 11 and extends.
Engaging claw 17 is positioned at the terminal part that respectively engages protuberance 13 on first.A side opposite with stiffener 16 sides in re-spective engagement protuberance 13 forms each engaging claw 17 on first.As shown in Figure 1B, each on first engaging claw 17 form hook-shapedly, and comprise the composition surface 17a that extend at the back side that is arranged essentially parallel to upper wall 11a, and connect composition surface 17a terminal part and the inclined-plane 17b that engages protuberance 13 terminal parts.The first inclined-plane 17b tilts like this, that is, along with its close upper wall 11a, inclined-plane 17b more leaves the side that engages protuberance 13.
As shown in Figure 1A and 1C, part reinforcement 11c is provided with engaging claw 19 on second.Each on second engaging claw 19 be positioned at corresponding reinforcement 11c with respect to base material 11 center longitudinally.As shown in Fig. 1 C, each engaging claw 19 forms hook-shaped, and comprises second composition surface 19a of the back side extension that is arranged essentially parallel to upper wall 11a and the inclined-plane 19b that connects composition surface 19a terminal part and corresponding reinforcement 11c terminal part.The second inclined-plane 19b tilts like this, that is, along with its close upper wall 11a, inclined-plane 19b more leaves the side of corresponding reinforcement 11c.
To the method that be used to make one goods 10 be described now.
The method that is used to make the one goods 10 of present embodiment comprises shaping processing that the surface that is used to make cover material spare 12 and base material 11 is combined into one and the trim process that is used to repair moulding cover material spare 12 edges.
At first explanation is shaped and processes.
In the processing that is shaped, use the in-mould clad material formation method that has adopted the mould 30 shown in Figure 1B and Fig. 1 C.Specifically, cover material spare 12 is configured as with the shape of base material 11 and conforms to, and is bonded on the base material 11.Mould 30 comprises that vertical layout is with upper mold section 30a and female die 30b closed and that open.When closed and unlatching mould 30, one of upper mold section 30a and female die 30b move with respect to another at least.What seen in Figure 1B vertically is mould closure/opening direction, that is, and and the direction of upper mold section 30a and female die 30b relative motion.Upper mold section 30a is corresponding to first module, and female die 30b is corresponding to second module.Upper mold section 30a respectively is configured to can realize being used to make cover material spare 12 closely to contact the application of vacuum on die joint (PL surface) with female die 30b.Upper mold section 30a comprises cavity surface, and this cavity surface forms corresponding to the surface of one goods 10 (combination with decorative surfaces).
As shown in Figure 1B, each first locking protuberance 32 protrudes upward from the bottom of corresponding recess 31a, and has and engage first time engaging claw 33 of protuberance 13 joints.Each first time engaging claw 33 forms hook-shaped, and comprise the first contact surface 33a and the first inclined surface 33b, the first contact surface 33a extends along horizontal plane basically, with the composition surface 17a of contact joint protuberance 13, the first inclined surface 33b connects the terminal part of contact surface 33a and the terminal part of the first locking protuberance 32.Each first inclined surface 33b tilts like this, that is, along with its close lower end, the first inclined surface 33b more leaves locking protuberance 32.
As shown in Fig. 1 C, each second locking protuberance 36 protrudes upward from the bottom of corresponding recess 31a, and have with base material 11 second on second time engaging claw 37 engaging of engaging claw 19.As under the situation of first time engaging claw 33, each second time engaging claw 37 forms hook-shaped, and comprise second contact surface and second inclined surface, second contact surface extends along horizontal plane basically, to contact the second composition surface 19a, second inclined surface connects the terminal part of this contact surface and the terminal part of the second locking protuberance 36.Each second inclined surface tilts like this, that is, along with its close lower end, this second inclined surface more leaves locking protuberance 36.
In the present embodiment, be located at engaging claw 17 on first on the joint protuberance 13 of base material 11 and first time engaging claw 33 of being located in the first locking protuberance 32 of female die 30b forms first detent mechanism.In addition, be located at engaging claw 19 and second second time engaging claw, 37 formation, second detent mechanism that locks in the protuberance 36 that is located at female die 30b on second on the base material 11.
When adopting mould 30 to carry out in-mould clad material formation method, base material 11 is placed on the female die 30b.At this moment, as shown in Figure 1B, the inner surface of the back side of upper wall 11a and sidewall 11b all contacts pedestal 31.This has just determined the position of base material 11 with respect to female die 30b at vertical and horizontal.In addition, as shown in Figure 1B and Fig. 1 C, engaging claw 19 all enters corresponding recess 31a on reinforcement 11c, the bump bonding 13 and second.
When each engaged protuberance 13 and enters corresponding recess 31a, when the inclined surface 33b of locking protuberance 32 slided, each engaged protuberance 13 strains takes place at the first inclined-plane 17b.After this, when the composition surface 17a of joint protuberance 13 contact first locked the contact surface 33a of protuberance 32, the strain that engages protuberance 13 disappeared, and joint protuberance 13 returns to original shape.As a result, engaging protuberance 13 engages with the first locking protuberance 32 of female die 30b.
On the other hand, when each when engaging claw 19 enters corresponding recess 31a on second, when the inclined surface of the corresponding second locking protuberance 36 slided, the reinforcement 11c appropriate section that engaging claw 19 on second is connected to upper wall 11a deformed at the second inclined-plane 19b.After this, when the composition surface 19a of engaging claw on second 19 contact second locked the contact surface of protuberance 36, the strain of reinforcement 11c disappeared, and reinforcement 11c returns to original shape.As a result, engaging claw 19 engages with the second locking protuberance 36 of female die 30b on second.
When as mentioned above, be located at when engaging claw 19 engages with the locking protuberance 32,36 of female die 30b on the turning of upper wall 11a and the joint protuberance 13 and second in the core, any position in comprising the plane of vertical and horizontal, the upper surface of upper wall 11a is positioned at suitable height with respect to female die 30b.Therefore, the vertical position on base material 11 surfaces is determined in any position in comprising the plane of vertical and horizontal with respect to female die 30b.Because engaging protuberance 13 is two row with lateral arrangement longitudinally, so the relative position that engages between the protuberance 13 allows to determine the position of base material 11 with respect to female die 30b at vertical and horizontal.Therefore, according to the in-mould clad material formation method of present embodiment, in vertical, horizontal and vertical whole directions, determine the position of base material 11 surfaces with respect to female die 30b.Vertically corresponding to mould closure/opening direction, that is, and the direction of upper mold section 30a and female die 30b relative motion.
Then, clamp the relative both sides of size, and be heated softening greater than the cover material spare 12 of base material 11 sizes.Softening cover material spare 12 is positioned between base material on the female die 30b 11 and upper mold section 30a.After this, from the PL surface of upper mold section 30a cover material spare 12 is vacuumized, so that the surface of cover material spare 12 (combination with decorative surfaces) closely contacts the cavity surface of upper mold section 30a.At this moment, if the cavity surface of upper mold section 30a has satin shape tissue or texture, then this pattern can be transferred on the surface of cover material spare 12.
After this, the PL of upper mold section 30a and female die 30b surface contacts, and the edge clamping of cover material spare 12 is between upper mold section 30a and female die 30b simultaneously.Subsequently, from the PL surface of female die 30b cover material spare 12 is vacuumized, so that the surface and the female die 30b of cover material spare 12 tight contact substrates 11.After this, closed upper mold section 30a and female die 30b.As a result, in mould 30, form the one goods 10 that base material 11 surfaces are bonded to cover material spare 12 back sides.
When one goods 10 during from mould 30 demouldings, as shown in Figure 2, cover material spare 12 becomes one with the surface of base material 11.In one goods 10, the peripheral part of cover material spare 12 is outstanding from the edge (lower end of sidewall 11b) of base material 11.Cover material spare 12 peripheral parts comprise folded part 12a and are positioned at the redundance 12b in the folded part 12a outside.Redundance 12b is included in the part of clamping in cover material spare 12 heating processes and is clipped in part between female die 30a, the 30b edge.Remove redundance 12b in trim process, this will be described below.
Below trim process will be described.
In trim process, use the anchor clamps 40 shown in Fig. 2.Anchor clamps 40 comprise the water spray cutter 40b that is used to support the support section 40a of one goods 10 and is used to remove redundance 12b.Water spray cutter 40b is positioned at the side of support section 40a.Water spray cutting 40b moves along the edge of the one goods 10 that supported by support section 40a, and blows High-Pressure Water to the base end part of redundance 12b, thereby removes redundance 12b.
Positioning element 44 is located on the upper surface of supporting base 41.Each positioning element 44 is corresponding to engaging one of protuberance 13.By means of the crimping section 45a that is fixed to the cylinder 45 on the supporting base 41,, on supporting base 41, determine the position of each positioning element 44 in vertical or horizontal.Each positioning element 44 has lock pawl 48 on top.Lock pawl 48 engages with the re-spective engagement protuberance 13 of base material 11.Each lock pawl 48 comprises the 3rd contact surface 48a of the level of being essentially.The 3rd contact surface 48a and re-spective engagement protuberance 13 first on the composition surface 17a of engaging claw 17 contact.The 3rd contact surface 48a of the lock pawl 48 of positioning element 44 and the composition surface 17a that is located at engaging claw 17 on first on the base material 11 joint protuberances 13 form the 3rd detent mechanism.
When using anchor clamps 40 to carry out trim process, one goods 10 are placed on the supporting base 41.At this moment, as shown in Figure 2, the back side of base material 11 upper wall 11a is held by pumping unit 42, and the sidewall 11b of base material 11 contacts with contact portion 43.Like this, with respect to the position of the support section 40a of anchor clamps 40,, locate the base material 11 of these one goods 10 about vertical and horizontal.
Next, the crimping section 45a of cylinder 45 extends along supporting base 41, so that the lock pawl 48 of each positioning element 44 engages with the re-spective engagement protuberance 13 of base material 11.At this moment, each composition surface 17a that engages protuberance 13 contacts with the composition surface 48a of lock pawl 48.When the joint protuberance 13 that is located at upper wall 11a corner engages with the lock pawl 48 of support section 40a, any position in comprising the plane of vertical and horizontal, the upper surface of upper wall 11a is positioned at suitable height with respect to support section 40a.Vertically be defined as direction perpendicular to upper wall 11a (upper surface of upper wall 11a and the back side).Therefore, the vertical position of the surface of one goods 10 with respect to support section 40a determined in any position in comprising the plane of vertical and horizontal.As a result, along the whole periphery of cover material spare 12, with respect to contact portion 43, marginal position between folded part 12a that vertically determines cover material spare 12 and redundance 12b.
All be arranged as two row owing to engage protuberance 13 at vertical and horizontal, so the relative position that engages between the protuberance 13 allows to determine the position of one goods 10 surfaces with respect to support section 40a at vertical and horizontal.Therefore, in the process of the trim process of present embodiment,,,, determine the marginal position between folded part 12a and the redundance 12b with respect to contact portion 43 along the whole periphery of cover material spare 12 in vertical, horizontal and vertical whole directions.
Then, replace shown in the chain-dotted line,, remove the redundance 12b that is placed on the one goods 10 on the support section 40a by means of water spray cutter 40b as the length among Fig. 2.At this moment, because in vertical, horizontal and vertical whole directions, determine the position of one goods 10 with respect to support section 40a, the redundance 12b by means of water spray cutter 40b removes cover material spare 12 keeps the folded part 12a with constant width at base material 11 peripheries simultaneously.At last, take off one goods 10 from support section 40a.Then, the folded part 12a of cover material spare 12 is bonded on the lower surface of base material 11 sidewall 11b, thereby finishes the one goods 10 shown in Figure 1A.
Above embodiment has following advantage.
According to in-mould clad material formation method according to present embodiment, when being placed on base material 11 in the mould 30, first and second detent mechanisms, any position in comprising the vertical and horizontal plane is with the be positioned at predetermined altitude of base material 11 surfaces with respect to female die 30b.Therefore, the surface of base material 11 is in the pre-position of vertical and horizontal, and 30a is positioned at predetermined altitude with respect to upper mold section.As a result, cover material spare 12 is arranged in the appropriate location between base material 11 surfaces and the upper mold section 30a, and is combined into one with the surface of base material 11.Therefore, after bonding, cover material spare 12 is difficult for fold or fracture.Thereby the defective that can reduce one goods 10 produces.Can improve productive rate thus.
Particularly, when forming base material 11, might cause variation, for example warpage in vertical dimensional accuracy by injection moulding.Can proofread and correct this variation reliably by detent mechanism.In addition, under these circumstances, that is, under the situation of number with weight reduction of thickness that reduces base material 11 (upper wall 11a) or minimizing reinforcement 11c, the variation of dimensional accuracy may take place owing to the warpage of base material 11.The detent mechanism of present embodiment is particularly suitable for this situation.
In addition, in the one goods 10 of present embodiment, the surface of base material 11 and on below the base material 11 distance between composition surface 17a, the 19a of engaging claw 17,19, significantly less than the vertical and horizontal size of base material 11, the precision of this vertical and horizontal size reduces easily.In injection moulding base material 11, the warpage major part occurs in and forms among the flat upper wall 11a, and rare in the joint protuberance 13 of reinforcement 11c.Therefore, last engaging claw 17,19 surfaces with respect to base material 11 have high dimension precision.Like this,, determine the height of base material 11 surfaces, can reduce the defective appearance and improve productive rate with respect to female die 30b by detent mechanism by means of engaging claw 33,37 under last engaging claw 17,19 that comprises base material 11 and the female die 30b.
According to the in-mould clad material formation method of present embodiment, engage with locking protuberance 32,36 by making engaging claw 17,19, detent mechanism is in the vertical position of determining base material 11 surfaces with respect to female die 30b.Last engaging claw 17,19 separates on the surface of vertical and base material 11.Like this, when last engaging claw 17,19 engages with locking protuberance 32,36, can be easily in the vertical position of determining base material 11 surfaces with respect to locking protuberance 32,36.
According to the method that is used to make one goods 10, this in-mould clad material formation method prevents made cover material spare 12 fold or fracture in the process of processing that is shaped.In trim process, base material 11 first on engaging claw 17 engage with the lock pawl 48 of anchor clamps 40, thereby support section 40a with respect to anchor clamps 40, any position in comprising the plane of vertical and horizontal, with the predetermined altitude that is positioned at of cover material spare 12, at this moment the cover material spare 12 that combines with base material 11 is repaired.Therefore, above method helps to produce high-quality one goods 10, and wherein cover material spare 12 can fold or fracture, and has along the peripheral part of the preset width of base material 11 peripheries.Therefore, can reduce defective appearance and raising productive rate.
Can as described below preferred embodiment be changed.
Can save four to three of engaging in the protuberance 13 of base material 11.Joint protuberance 13 can be positioned at any position on the upper wall 11a back side.Engage protuberance 13 and be preferably placed at vertical two ends, so that make any position in comprising the plane of vertical and horizontal, in the vertical position of determining base material 11 surfaces with respect to female die 30b, and make in the position of vertically definite base material 11 surfaces with respect to female die 30b.
Each first and second detent mechanism can comprise the engagement device of any kind, as long as this mechanism allows vertically to locate base material 11 surfaces with respect to the position of female die 30b.Equally, each of each the 3rd detent mechanism can comprise the engagement device of any kind, as long as this mechanism allows vertically to locate base material 11 surfaces with respect to the support section 40a of anchor clamps 40.
Can save first detent mechanism or second detent mechanism.If save first detent mechanism, then preferably, at least one pair of on second engaging claw 19 be positioned at vertically each end of base material 11 so that any position in comprising the plane of vertical and horizontal, with respect to base material 11 surfaces, vertical location of female die 30b.
Except that the 3rd contact surface 48a of the positioning element 44 of anchor clamps 40, the support section 40a of anchor clamps 40 can be provided with another contact surface that engages with the composition surface 19a of engaging claw 19 on the base material 11 second.Can save the 3rd composition surface 48a, thereby, can have only the contact surface that engages with composition surface 19a to be arranged on the support section 40a of anchor clamps 40.
In illustrative embodiments, mould 30 comprises last female die 30a, the 30b of vertical layout.Yet, also can use side direction (laterally) to open and closed mould.
The structure that can adopt mould 30 to put upside down.Specifically, the upper mold section 30a of illustrative embodiments can be positioned at the below of female die 30b, and can vertically closed and unlatching half module 30a, 30b.In this case, should suitably explain vertical, vertical and horizontal in the illustrative embodiments according to the relative position of last female die 30a, 30b and closing direction.
In illustrative embodiments, the supporting base 41 of anchor clamps 40 is orientated level.Yet supporting base 41 also can be vertical orientation.
The anchor clamps 40 of illustrative embodiments can be put upside down.Specifically, one goods 10 can be positioned at the below of the supporting base 41 of illustrative embodiments.In this case, should suitably explain vertical, vertical and horizontal in the illustrative embodiments according to the relative position of anchor clamps 40 and base material 11.
Claims (7)
1. one kind is used for making the cover material spare and the surface of base material to form the in-mould clad material formation method of one at mould, described mould comprises first module and second module, wherein, at least one of described first module and second module can move with respect to another at the mould moving direction, and described in-mould clad material formation method is characterised in that:
On described second module, described base material is set, makes the back side of described base material relative with described second module;
When described base material is set,, locate the surface of described base material with respect to described second module at described mould moving direction by the detent mechanism between the back side of described second module and described base material;
Described cover material spare is positioned over described first module and is arranged between the described base material on described second module; And
By application of vacuum described cover material spare is pressed against on the described base material, simultaneously,, the described cover material spare and the surface of described base material is combined into one by with respect to closed described first module of described second module.
2. in-mould clad material formation method according to claim 1, it is characterized in that, described surface of locating described base material at described mould moving direction with respect to described second module, comprise: by described detent mechanism, make the back side of described base material engage one another, thereby stop described base material to separate from described second module at described mould moving direction with described second module.
3. in-mould clad material formation method according to claim 1 is characterized in that, described detent mechanism comprises the engaging claw on the locking protuberance that is located on described second module and the back side that is located at described base material,
Wherein, describedly locate the surface of described base material with respect to described second module, comprising: under the state that described base material is arranged on described second module, make described engaging claw engage with described locking protuberance at described mould moving direction.
4. in-mould clad material formation method according to claim 3 is characterized in that, described engaging claw engages with described locking protuberance, thereby stops described base material to separate from described second module at described mould moving direction.
5. in-mould clad material formation method according to claim 3, it is characterized in that, describedly make described engaging claw engage with described locking protuberance, comprise: make the composition surface of described engaging claw engage with contact surface on being located at described locking protuberance, the composition surface of described engaging claw and described mould moving direction intersect.
6. according to the claim 1 described in-mould clad material of each claim formation method to the claim 5, it is characterized in that, described surface of locating described base material at described mould moving direction with respect to described second module, comprise: in a plurality of positions, by a plurality of detent mechanisms between the back side of described second module and described base material, locate the surface of described base material with respect to described second module at described mould moving direction.
7. method that is used to make clad material integrated shaped product, wherein, cover material spare is combined into one with the surface of base material, and described method is characterised in that:
Make the described cover material spare and the surface of described base material in mould, form one, described mould comprises first module and second module, and wherein, one of described at least first module and second module can move with respect to another, wherein, described described cover material spare comprises with the surface formation one of described base material:
On described second module, described base material is set, makes the back side of described base material relative with described second module;
When described base material is set,,,, locate the surface of described base material with respect to described second module at described mould moving direction by making the engaging claw on the back side be located at described base material engage with locking protuberance on being located at described second module;
Described cover material spare is positioned over described first module and is located between the described base material on described second module; And
By application of vacuum described cover material spare is pressed against on the described base material, simultaneously,, the described cover material spare and the surface of described base material is combined into one by with respect to closed described first module of described second module; And
Under state by the back side of the described base material of fixture support, repair the edge of described cover material spare along the peripheral part of described base material, wherein, described anchor clamps comprise the lock pawl that can engage with described engaging claw, wherein, in described dressing process,, locate described base material with respect to described anchor clamps by making described engaging claw engage with described lock pawl.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2005217938A JP4525513B2 (en) | 2005-07-27 | 2005-07-27 | Manufacturing method of skin integral molding |
| JP2005217938 | 2005-07-27 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1903552A true CN1903552A (en) | 2007-01-31 |
| CN100591512C CN100591512C (en) | 2010-02-24 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN200610103810A Active CN100591512C (en) | 2005-07-27 | 2006-07-27 | In-mould clad material forming method, and method for manufacturing clad material integrated shaped product |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US7695670B2 (en) |
| JP (1) | JP4525513B2 (en) |
| CN (1) | CN100591512C (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104057430A (en) * | 2014-05-04 | 2014-09-24 | 宁波市鄞州永佳电机工具有限公司 | Tool box for storing sculpture cutters |
| US11975782B2 (en) | 2018-12-18 | 2024-05-07 | Honda Motor Co., Ltd. | Decorative molded component |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4525513B2 (en) * | 2005-07-27 | 2010-08-18 | 豊田合成株式会社 | Manufacturing method of skin integral molding |
| TWI394455B (en) * | 2009-01-23 | 2013-04-21 | Qisda Corp | An adjustable supporting structure and the display device comprising the adjustable supporting structure |
| JP5905288B2 (en) * | 2012-02-13 | 2016-04-20 | 株式会社ブリヂストン | Manufacturing method of mold and foam molding |
| US10179435B2 (en) | 2012-07-10 | 2019-01-15 | U.S. Farathane Corporation | Roof ditch molding assembly and process with heated air assist |
| US10071522B2 (en) * | 2012-07-10 | 2018-09-11 | U.S. Farathane Corporation | Roof ditch molding process incorporating conformed shaping features in a molding fixture |
| JP6859822B2 (en) * | 2017-04-14 | 2021-04-14 | トヨタ紡織株式会社 | Resin molded product and its manufacturing method |
| CN113039055B (en) * | 2018-12-18 | 2023-01-17 | 本田技研工业株式会社 | Decorative shaped article |
| CN215473608U (en) * | 2018-12-18 | 2022-01-11 | 本田技研工业株式会社 | External member |
| JP7210631B2 (en) * | 2021-03-31 | 2023-01-23 | 本田技研工業株式会社 | Method for manufacturing decorative molded product |
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| US2788048A (en) * | 1954-04-29 | 1957-04-09 | Harold E Kimes Corp | Metallic inserts for tires |
| JPS6250110A (en) * | 1985-08-29 | 1987-03-04 | Toyoda Gosei Co Ltd | Mold for insert molding |
| JPH03286834A (en) * | 1990-04-03 | 1991-12-17 | Nippon Plast Co Ltd | Method of sticking skin object to core |
| JPH07205167A (en) * | 1994-01-20 | 1995-08-08 | Inoac Corp | Skin fixing device in integral molding of skin |
| JP3514010B2 (en) * | 1995-10-04 | 2004-03-31 | 日本プラスト株式会社 | Soft resin molded product having an insert, insert mold used for molding the same, and method of manufacturing the same |
| US6120274A (en) * | 1997-11-26 | 2000-09-19 | Donnelly Corporation | Mold assembly for molding a remotely located attachment member on a sheet of material |
| US7108101B1 (en) * | 1998-09-14 | 2006-09-19 | Poly-Tec Products, Inc. | Manhole insert for manufacture of a cast member and to provide a step insert having increased structural and holding strength |
| JP2001179759A (en) | 1999-12-22 | 2001-07-03 | Kasai Kogyo Co Ltd | Method for molding laminated molding and molding device |
| JP2001205167A (en) | 2000-01-31 | 2001-07-31 | Aoi Chemical Inc | Simple seal instrument |
| JP2001252929A (en) * | 2000-03-08 | 2001-09-18 | Inoac Corp | Method and structure for fixing base material to foaming mold |
| JP4525513B2 (en) * | 2005-07-27 | 2010-08-18 | 豊田合成株式会社 | Manufacturing method of skin integral molding |
-
2005
- 2005-07-27 JP JP2005217938A patent/JP4525513B2/en active Active
-
2006
- 2006-07-25 US US11/492,228 patent/US7695670B2/en active Active
- 2006-07-27 CN CN200610103810A patent/CN100591512C/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104057430A (en) * | 2014-05-04 | 2014-09-24 | 宁波市鄞州永佳电机工具有限公司 | Tool box for storing sculpture cutters |
| US11975782B2 (en) | 2018-12-18 | 2024-05-07 | Honda Motor Co., Ltd. | Decorative molded component |
Also Published As
| Publication number | Publication date |
|---|---|
| US7695670B2 (en) | 2010-04-13 |
| US20070075464A1 (en) | 2007-04-05 |
| CN100591512C (en) | 2010-02-24 |
| JP4525513B2 (en) | 2010-08-18 |
| JP2007030380A (en) | 2007-02-08 |
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